NASA NTRS · 19630010614
AN APPROXIMATE METHOD FOR COMPUTING ERROR COEFFICIENT MATRICES FOR LUNAR TRAJECTORIES
Abstract
Problems in computing transition matrices of lunar trajectories
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Mc Lean, J. D.. 1963-01-01. AN APPROXIMATE METHOD FOR COMPUTING ERROR COEFFICIENT MATRICES FOR LUNAR TRAJECTORIES. https://ntrs.nasa.gov/citations/19630010614
Cite the original work for its findings. Save a collection to share your selection of sources.